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Wind-tunnel Investigation of Horizontal Tails IV : Unswept Plan Form of Aspect Ratio 2 and a Two-dimensional Model (1948)
NASA Technical Reports Server (NTRS) · leaf 44
MCA RM No. a8J21 … (a) Lift coefficient. Figure !4.- Section lift, hinge-moment, and pitching-moment coefficients of the NACA 64A0I0 airfoil. R,5.5xi0^.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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